Derivation of proper time in acceleration in SR

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The discussion centers on the derivation of proper time in the context of special relativity (SR) and the challenges associated with equations of motion under constant acceleration. Participants highlight discrepancies in equations relating coordinate and proper acceleration, noting that the coordinate acceleration is smaller by a factor of gamma cubed compared to proper acceleration. There is confusion regarding the use of trigonometric versus hyperbolic functions in these derivations, with suggestions that hyperbolic sine should be employed instead of sine. The conversation emphasizes the importance of using standard symbols to avoid misinterpretation and seeks clarity on the transition from momentum equations to proper acceleration relationships. Overall, the thread aims to resolve misunderstandings in the mathematical treatment of accelerated motion in relativistic contexts.
  • #31
yuiop said:
In the CMIRF, the acceleration is a' = dv'/dt = dx'/dt'2. Now dx = dx'/\gamma and dt2 = dt'2*\gamma^2, so after substitutions a = dv/dt = dx/dt2 = (dx'/dt'2)//\gamma^3

The force required to accelerate a particle parallel to its velocity increases significantly as the velocity increases and this gamma cubed factor is routinely observed in particle accelerators. This leads to a diminishing law of returns for particle accelerators. To attain terminal velocities that are 1% higher than the terminal velocity of the CERN accelerator particles, would require an accelerator that is orders of magnitude more expensive to build and operate. However, it is still worth their while investing in larger accelerators because the energy levels of the collisions are significantly higher, for what looks like a small increase in velocity.
.

Hiyuiop My first reaction to your post was "wonderful", one of those few questions with a neat definitive empirical answer. But having though it over I have more questions.
In the accelerator tests do they actually do a coordinate acceleration profile based on short interval velocities, during the course of acceleration??
I would assume they would have no imperative to maintain constant proper acceleration for the electrons but would just go for the flattest . most constant coordinate acceleration obtainable . yes??
SO does the gamma cubed factor relate to the energy required to maintain maximal acceleration or is it also a declining acceleration curve?
The above derivation, not surprisingly makes complete sense but...
it is based on acceleration relative to an abstract CMIRF and then this is transformed into rest frame coordinate acceleration at the end. This may of course be absolutely valid but it seems to me that in this circumstance the CIMRFs are somewhat of a bootstrap construct i.e. accelerating relative to one and then there is automatically another one there to accelerate from , with no direct connection to the observation from the reference frame , of either the acceleration of the actual system or the acceleration of the CMIRF.
The increased velocity is just assumed. The coordinate acceleration in the reference frame would actually have to be based on a series of short interval "instantaneous" velocity measurements , no?

Maybe a little more thought on my part.
Thanks for the info
 
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  • #32
Passionflower said:
You can render Excel formulas or hand-typed Latex directly in Excel by using:

http://www.codecogs.com/components/excel_render/excel_install.php

That way you can keep the formulas and the Latex close together!

Thanks Passionflower. Nice tip. :smile:

starthaus said:
This is incorrect, the units are all wrong because you missed a c^2 in calculating the derivative.

Thanks Starthaus. Your right. I have fixed the original in post #24 and inserted the missing c^2.
 
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  • #33
starthaus -

in your post, #29, where did you get the yuiop quote from (your hyperlink leads to post 24 from yuiop) because in post 24, he has a/c2 which, as you correctly pointed out, makes things come out correctly

F = mdv/dt\gamma^3
= \gamma^3ma
 
  • #34
yuiop said:
Problem statement:

Proper acceleration = 2c /s.

The x axes of S and S' are parallel to each other and the relative velocity of the frames and the acceleration and the velocity of the accelerated object is parallel to the x axes.

The velocity of accelerating object is v=0 at time t=0 and the object accelerates for 10 seconds as measured in frame S. We will consider two events, one at the start and at one at the end of the acceleration period.

Event 1:
(x1,t1) = (0,0)
(x1',t2') = (0,0)

Event 2:
(x2,t2) = (Δx,10)
(x2',t2') = (Δx', Δt')
Another interesting titbit is the question what is the slowest time to go from Event 1 to Event 2?

It turns out to be around 3.084 Years. In other words the traveler took a 40% shortcut 'through' spacetime.
 
  • #35
stevmg said:
starthaus -

in your post, #29, where did you get the yuiop quote from (your hyperlink leads to post 24 from yuiop) because in post 24, he has a/c2 which, as you correctly pointed out, makes things come out correctly

F = mdv/dt\gamma^3
= \gamma^3ma

He fixed it, see post 32.
 
  • #36
yuiop,
In post 28 (cited below) you point out that you derived in post 8.
v = \frac{a't}{\sqrt{1+(a't/c)^2}}

a' is the acceleration in S'.

But you actually derived a in that post (the acceleration in S, not S') I have included that post 8 below this post 28 below

Now, based on the original a and final t, what did you do?

I am lost.

Post 28, yiuop
yuiop said:
In post #8 I derived:

v = \frac{a't}{\sqrt{1+(a't/c)^2}}
Substitute this for the v in \gamma = 1/\sqrt{1-v^2/c^2} and you eventually get after some algebraic manipulation:

\gamma = \sqrt{1 + (a't/c)^2}

I see you have already done the numerical example for t=10 and v=0.99875c in S and a proper acceleration of 2c per second in your edit. Just for clarity, here is another example for the event t=1 in S. At this event the velocity is:

v = \frac{a't}{\sqrt{1+(a't/c)^2}} = \frac{2}{\sqrt{1+(2)^2}} = 0.8944c

The gamma factor at time t=1 and v = 0.8944c in S is:

\gamma = \sqrt{1 + (a't/c)^2} = \sqrt{1+2^2} = 2.2361

or

\gamma = \frac{1}{\sqrt{1 - v^2/c^2}} = \frac{1}{\sqrt{1-0.8944^2}} =2.2361

Well done. You have found another typo. :-p It should have been:

v = \frac{a't}{\sqrt{1+(a't/c)^2}} = \frac{a't}{\gamma} = \frac{2*10}{20.025} = 0.99875c

where a'=2 and t=10 as given in S and the gamma factor of 20.025 was calculated earlier.

Yes, as in the title of the paragraph.

Sorry about the typos in the equations. I know the numbers are right because I did them in a spreadsheet, but the hassles of entering and previewing TEX equations means some errors sometimes creep in during the translation. At least this this is a two way medium and we can get right between us. :wink:

Post 8, yiuop
yuiop said:
As I mentioned in post #2, the coordinate acceleration is a factor of gamma cubed smaller than the proper acceleration. In the last two equations above, capital T is the coordinate time and small t is the proper time, but to avoid further confusion I will use the symbols recommended by Passionflower, so that:

a = \frac{dv}{dt} = \alpha \gamma^{-3} = \alpha (1-v^2/c^2)^{3/2}

This can be rearranged to:

\frac{dt}{dv} = \frac{1}{\alpha(1-v^2/c^2)^{3/2}}

Integrating both sides with respect to v gives:

t= \int \left( \frac{1}{\alpha(1-v^2/c^2)^{3/2}} \right) dv = \frac{v}{\alpha \sqrt{1-v^2/c^2}}

When rearranged:

v= \alpha t \sqrt{1-v^2/c^2}

\rightarrow v^2 = (\alpha t)^2 - (\alpha t v/c)^2

\rightarrow v^2 (1+ (\alpha t /c)^2) = (\alpha t)^2

\rightarrow v = \frac{\alpha t}{\sqrt{1+(\alpha t/c)^2}}
which is the last equation you asked about in your post.
 
  • #37
stevmg said:
yuiop,
In post 28 (cited below) you point out that you derived in post 8.
v = \frac{a't}{\sqrt{1+(a't/c)^2}}

a' is the acceleration in S'.

But you actually derived a in that post (the acceleration in S, not S') I have included that post 8 below this post 28 below

Now, based on the original a and final t, what did you do?

I am lost.

In post 8, I was using the alpha symbol \alpha to represent proper acceleration measured by an accelerometer on the accelerating rocket. (click on the latex symbol to see the underlying code). By post 28 the symbol I was using for proper acceleration was a_0 to identify the measurement made by the accelerating observer in a consistent way. The proper acceleration is numerically equal to the (give or take a sign) to the coordinate acceleration measured by the CMIRF observer so \alpha, a' and a_0 are equivalent and interchangeable. So the coordinate acceleration a is related to the others by a = a'\gamma^3 = a_0\gamma^3 = \alpha \gamma^3. Like you said, lots of observers so lots of symbols required.

So given:

v = \frac{a_0t}{\sqrt{1+(a_0t/c)^2}}

and substitute into \frac{1}{\gamma} = \sqrt{1-v^2/c^2}

you get:

\frac{1}{\gamma} = \sqrt{1-\frac{(a_0t/c)^2}{(1+(a_0t/c)^2)}}= \sqrt{\frac{1+(a_0t/c)^2-(a_0t/c)^2}{(1+(a_0t/c)^2)}}=<br /> {\frac{1}{\sqrt{1+(a_0t/c)^2}}

\rightarrow \gamma = \sqrt{1+(a_0t/c)^2}}
 
  • #38
Passionflower said:
Another interesting titbit is the question what is the slowest time to go from Event 1 to Event 2?

It turns out to be around 3.084 Years. In other words the traveler took a 40% shortcut 'through' spacetime.

While checking out your observation, I noticed another interesting relationship.

The slowest time between the two events is the elapsed proper time interval t_i measured by a clock moving inertially between the two events, i.e. t_i = \sqrt{\Delta t^2 - \Delta x^2/c^2}

Now it seems from playing around with my spreadsheet, that the following (without proof) is true:

\Delta x = \frac{1}{2} \alpha t_i^2

which has the same form as the Newtonian equation.

It obviously follows that the constant proper acceleration can be obtained from this simple equation:

\alpha = 2\frac{\Delta x}{t_i^2}

P.S. That should be seconds, not years, to be consistent with the original scenario :wink:
 
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  • #39
Austin0 said:
Hiyuiop My first reaction to your post was "wonderful", one of those few questions with a neat definitive empirical answer. But having though it over I have more questions.
In the accelerator tests do they actually do a coordinate acceleration profile based on short interval velocities, during the course of acceleration??
I would assume they would have no imperative to maintain constant proper acceleration for the electrons but would just go for the flattest . most constant coordinate acceleration obtainable . yes??
I have no knowledge about the practical design and operation of particle accelerators. Maybe someone like ZapperZ can help you with this.

Although there is as far as know, no imperative to go for constant proper acceleration, it is entirely natural to do so, because that is what happens naturally when you apply a constant force in the accelerator frame. This would seem the simplest option, rather than applying a progressively increasing force trying to maintain a constant coordinate acceleration.

Also, AFAIK there are accelerating sections in the ring and constant speed sections where they carry out the experiments e.t.c. As the particles go around the ring, the energy to the accelerating section has to to be timed to coincide with the arrival of a bunch of particles at the accelerating section of the ring. This requires knowledge of the exact velocity and location of the particles in the ring at all times and this requires using relativistic calculations. If they used Newtonian calculations, the timing would be significantly out and the accelerator simply wouldn't work. The magnitude of relativistic effects in a particle accelerator is far greater than the often quoted example of GPS satelites.
Austin0 said:
SO does the gamma cubed factor relate to the energy required to maintain maximal acceleration or is it also a declining acceleration curve?
As above, my guess is a declining coordinate acceleration curve, but I am ready to concede to any real experts on the subject.

Austin0 said:
The above derivation, not surprisingly makes complete sense but...
it is based on acceleration relative to an abstract CMIRF and then this is transformed into rest frame coordinate acceleration at the end. This may of course be absolutely valid but it seems to me that in this circumstance the CIMRFs are somewhat of a bootstrap construct i.e. accelerating relative to one and then there is automatically another one there to accelerate from , with no direct connection to the observation from the reference frame , of either the acceleration of the actual system or the acceleration of the CMIRF.
The increased velocity is just assumed. The coordinate acceleration in the reference frame would actually have to be based on a series of short interval "instantaneous" velocity measurements , no?

Maybe a little more thought on my part.
Thanks for the info

If we ask the question, "What happens if we accelerate an object that is already moving at 0.9c?", the initial analysis might seem daunting. Here is one way of thinking about it that might help. Consider a car that accelerates from 0 to 180 mph in 6 seconds. That is quick for a car, but the relativistic effects are insignificant and can be ignored and we can use Newtonian equations and be correct to a high order of accuracy. To know hat happens if the car was initially traveling at 0.9c and then accelerated with the same force (measured by the car accelerometer) then the relativity principle tells us that all we have to do is do a Lorentz transformation of our car to the point of view of an inertial observer going past us at -0.9c. When we do that, the gamma cubed factor comes out. To build a complete picture then you are right that we need a whole series of observers with velocities varying by an infinitesimal step size. The 180 mph and 5 second figures are arbitrary and I was just trying to demonstrate that the infinitesimal steps assumed by integration, do not actually have to be that small in practice, to get a reasonably accurate result.
 
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  • #40
yuiop said:
While checking out your observation, I noticed another interesting relationship.

The slowest time between the two events is the proper time t_i by a clock moving inertially between the two events, i.e. t_i = \Delta t^2 - \Delta x^2/c^2

You must mean

d \tau=\sqrt{ \Delta t^2 - \Delta x^2/c^2}

Now it seems from playing around with my spreadsheet, that the following (without proof) is true:

\Delta x = \frac{1}{2} \alpha t_i^2

This cannot be since:

x=\frac{c^2}{a}(cosh(a \tau/c)-1)

dx=c d\tau sinh(a \tau/c)

which has the same form as the Newtonian equation.

Maybe as an approximation but not in reality (see above)
It obviously follows that the constant proper acceleration can be obtained from this simple equation:

\alpha = 2\frac{\Delta x}{t_i^2}

No. See above.
 
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  • #41
yuiop said:
Coordinate distance Δx traveled in frame S

\Delta x = (c^2/a)*(\sqrt{(1+(a \Delta t /c)^2)} -1) = (c^2/a)*(\gamma-1) = (1/2)*(20.025-1) = 9.5125

I never actually derived the equation for coordinate distance above, so here it is.

The relativistic equation for kinetic energy is:

KE = \sqrt{(mc^2)^2 + (mcv\gamma)^2} - mc^2

This is the total energy that has been added to the particle that is accelerated from rest to v.

The work done on the particle is:

W = F\Delta x = ma\gamma^3 \Delta x = ma_0 \Delta x

Since the work is an expression for energy and is equal to the final kinetic energy of the accelerated particle (in a 100% efficient accelerator) then the two above equations can be equated as:

ma_0 \Delta x = \sqrt{(mc^2)^2 + (mcv\gamma)^2} - mc^2


\rightarrow \Delta x = \frac{ \sqrt{(c^2)^2 + (cv\gamma)^2} - c^2}{a_0}

\rightarrow \Delta x = (c^2/a_0) ( \sqrt{1 + (v\gamma/c)^2} - 1)

In an earlier post it was shown that v\gamma = a_0\Delta t and this is substituted into the above equation to obtain:

\Delta x = (c^2/a_0) ( \sqrt{1 + (a_\Delta t/c)^2} - 1)}

There are probably easier ways to derive it, but I thought it would be nice to introduce the relationships between force, energy and acceleration.
 
  • #42
starthaus said:
You must mean

t_i =\sqrt{ \Delta t^2 - \Delta x^2/c^2}

Yes, that is what I meant. (Fixed the original.) Thanks :wink:
starthaus said:
This cannot be since:

x=\frac{c^2}{a}(cosh(a \tau/c)-1)

dx=c d\tau sinh(a \tau/c)
The tau in the equations you have quoted is the proper time of the accelerating object moving between the two events. This is not the same as the proper time t_i that I was using, which is the proper time of an inertially moving object (with constant velocity) between the same two events. To try and avoid confusion, I did not use tau, because we are already using that for the proper time of the accelerating object.

As Passionflower pointed out, the elapsed proper time measured by the accelerating clock moving between the two events is about 40% of the elapsed proper time measured by an inertial clock that is present at the same two events.
starthaus said:
yuiop said:
Now it seems from playing around with my spreadsheet, that the following (without proof) is true:

\Delta x = \frac{1}{2} \alpha t_i^2

which has the same form as the Newtonian equation.

Maybe as an approximation but not in reality (see above)

No, it is intended to be exact, when the correct time measurement is used.
 
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  • #43
yuiop said:
Yes, that is what I meant. (Fixed the original.) Thanks :wink:

Well, your t_i as defined is the proper time of the accelerated observer.

The tau in the equations you have quoted is the proper time of the accelerating object moving between the two events. This is not the same as the proper time t_i that I was using,

The mathematical definition that you are using shows them to be one and the same.

No, it is intended to be exact, when the correct time measurement is used.

Try to do a derivation and let's see what you get.
 
  • #44
starthaus said:
Well, your t_i as defined is the proper time of the accelerated observer.

I defined \Delta t_i as \sqrt{\Delta t^2- \Delta x^2/c^2} in post #38:

This is directly obtained from the Minkowski metric and it is the elapsed proper time of a clock moving with constant velocity that is present at the two events, (0,0) and (x,t).

This is clearly not the same as the proper elapsed time \Delta \tau or \Delta t_0 of a clock with constant acceleration, that is present at the same two events. The elapsed proper time of the accelerating clock is defined by:

\Delta \tau = \Delta t_0 = \frac{c}{a_0}\, arsinh ( \frac{a_0 \Delta t}{c})\, = \, \frac{c}{a_0} \, arcosh({\frac{a_0 \Delta x}{c^2}+1)

It is easy to see that \Delta t_i \ne \Delta \tau because:\sqrt{\Delta t^2- \Delta x^2/c^2} \qquad \ne \qquad \frac{c}{a_0}\, arsinh ( \frac{a_0 \Delta t}{c})
and

\sqrt{\Delta t^2- \Delta x^2/c^2}\qquad \ne \qquad \frac{c}{a_0} \, arcosh({\frac{a_0 \Delta x}{c^2}+1)

starthaus said:
yuiop said:
The tau in the equations you have quoted is the proper time of the accelerating object moving between the two events. This is not the same as the proper time t_i that I was using, which is the proper time of an inertially moving object (with constant velocity) between the same two events.
The mathematical definition that you are using shows them to be one and the same.

I am afraid you are seriously mistaken about the maths and physics of this issue.
 
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  • #45
yuiop said:
I clearly defined t_i as \sqrt{\Delta t^2- \Delta x^2/c^2} in post #38

Yes. And this is not a very good definition to begin with because the RHS is a differential while the LHS is not.
This is directly obtained from the Minkowski metric and it is the elapsed proper time of a clock moving with constant velocity that is present at the two events, (0,0) and (x,t).

The standard interpretationfollows correctly from the INVARIANCE of the Minkowski metric as follows:

(c d \tau)^2=(cdt)^2-dx^2

I am sure I have shown you this before.
This is clearly not the same as the proper elapsed time \tau or t_0 of a clock with constant acceleration, that is present at the same two events. The elapsed proper time of the accelerating clock is defined by:

\tau = t_0 = \frac{c}{a_0}\, arcosh ( \frac{a_0 t}{c})\,

Yes, I just showed you this in the previous post.

=\frac{c}{a_0} \, arsinh{\frac{a_0 \Delta x}{c^2})

Definitely wrong since you are effectively writing t=\frac{\Delta x}{c}
It is easy to see that t_i \ne \tau because:\sqrt{\Delta t^2- \Delta x^2/c^2} \qquad \ne \qquad \frac{c}{a_0} arcosh ( \frac{a_0 t}{c})

Sure, if you use wrong derivations, it is easy to show anything. Do you understand the difference between \tau and d \tau? One is a variable, the other one is a differential, you are mixing them freely and incorrectly.
Speaking of derivations, where is the derivation for your claim that started this debate?
 
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  • #46
yuiop said:
I am going to introduce some new notation because of the complication that arise when considering the measurements according to the inertial observer with velocity relative to the accelerating observer, the accelerating observer and the co moving inertial observer.

Quantities that are proper measurements made by the accelerating observer will be denoted by zero subscript such as m0, t0 and a0.

Quantities measured by the inertial observer at rest in frame S with velocity relative to the accelerating observer do not have a subscript or a superscript, e.g. m, t and a.

Quantities measured in the Co-Moving Inertial Reference Frame (CMIIRF or S') will be denoted by a prime symbol, eg m', t' and a'.

m = m' = m0

a0 = a'

In earlier posts we have established with help from DrGreg that a = dv/dt = a'/γ3.

We have also established that

F = dp/dt = d(mvγ)/dt' = m d(vγ)/dt = may3 = ma'

and it is also true that:

F = may3 = m(dv/dt)y3 = m(a'/γ33 = ma'

From the above we can conclude that F = F' = F0 because in the co-moving frame where the v=0, F' = ma'γ3 = ma'*(sqrt(1-v2))3 = ma'*(sqrt(1-02))3 = ma'.

Unfortunately the values you have chosen for acceleration and the time period, means that relativistic effects are extremely small and barely distinguishable from Newtonian calculations.

Staying with the car metaphor, let's fit a performance exhaust, go-faster-stripes and nitro injection and boost the acceleration up to 2c per second and use units of c=1. Yes, surprisingly 2c per second is allowed, because 2c is the hypothetical terminal velocity that reached if it was possible to maintain a constant coordinate acceleration for a full second, which is of course impossible, but that sort of acceleration is in principle possible for an infinitesimal time period.

Problem statement:

Proper acceleration = 2c /s.

The x axes of S and S' are parallel to each other and the relative velocity of the frames and the acceleration and the velocity of the accelerated object is parallel to the x axes.

The velocity of accelerating object is v=0 at time t=0 and the object accelerates for 10 seconds as measured in frame S. We will consider two events, one at the start and at one at the end of the acceleration period.

Event 1:
(x1,t1) = (0,0)
(x1',t2') = (0,0)

Event 2:
(x2,t2) = (Δx,10)
(x2',t2') = (Δx', Δt')

\Delta x = (x_2-x_1) = x_2 \quad , \quad \Delta t = (t_2-t_1) = t_2
\Delta x&#039; = (x_2&#039;-x_1&#039;) = x_2&#039; \quad , \quad \Delta t&#039; = (t_2&#039;-t_1&#039;) = t_2&#039;

v is the final velocity of the accelerating object in frame S and is also the relative velocity of frame S' to frame S.

The instantaneous gamma factor at the terminal velocity in frame S

\gamma = \sqrt{1+(a&#039;t/c)^2} = \frac{1}{\sqrt{1-v^2/c^2}} = 20.025

Final coordinate velocity in S

v = \frac{a&#039;t}{\sqrt{1+(a&#039;t/c)^2}} = a&#039;t/\gamma = \frac{2*10}{20.025} = 0.99875c

Final coordinate acceleration in S

The initial coordinate acceleration is equal to the proper acceleration, but while the proper acceleration remains constant the coordinate acceleration does not and the final coordinate acceleration is:

a = a_0/\gamma^3 = 2/20.025^3 = 0.00025c/s

Final coordinate velocity in the CMIRF (S')

This is zero by definition. Note that the initial velocity in S' was -0.99875c.

Coordinate distance Δx traveled in frame S

\Delta x = (c^2/a)*(\sqrt{(1+(a \Delta t /c)^2)} -1) = (c^2/a)*(\gamma-1) = (1/2)*(20.025-1) = 9.5125

Coordinate distance Δx' in the CMIRF (S')

Fram the Lorentz transformation:

\Delta x&#039; = \frac{\Delta x-v \Delta t}{\sqrt{1-v^2/c^2}} = \gamma(\Delta x-v \Delta t) = 20.025*(9.5125-0.99875*10) = -9.5125

You might find it surprising and unintuitive that the distance between the two events is the same in frame S and frame S', except for the sign. I know I did and maybe I made a mistake somewhere.

Proper distance:

Distance is poorly defined in an accelerating reference frame. Proper distance in inertial RFs is normally the distance measured by a ruler between two simultaneous events. Since the two events are not simultaneous in any inertial reference frame in this example it is hard to define a proper distance even in the inertial reference frames. We can however invoke a notion of the invariant interval which can be thought of as the proper distance between events 1 and 2.

(c \Delta t)^2 - \Delta x^2 = (10)^2 - 9.5125^2 = 9.5125

This is invariant for any inertial reference frame (moving parallel to the x axis) but I am not sure if it applies to accelerating frames.

Coordinate elapsed time Δt' in the CMIRF

Using the Lorentz transformation:

\Delta t&#039; = \frac{<br /> \Delta t-v \Delta x/c^2}{\sqrt{1-v^2/c^2}} = \gamma(\Delta t-v\Delta x/c^2) = 20.025*(10-0.99875*9.5125) = 10 s

Again this is a counter-intuitive result.

Proper elapsed time:

The proper elapsed time for the accelerating object is clearly defined because it measured by a single clock between the two events. It is derived like this. The total elapsed proper time is the integral of the instantaneous proper time at any instant which is a function of the instantaneous velocity u at any instant, so:

\frac{dt_0}{dt} = \frac{1}{\gamma^2} = \sqrt{1-u^2/c^2} = \frac{1}{\sqrt{1+(a_0\Delta t/c)^2}}

Integrating both sides with respect to t:

\Delta t_0 = \int \left( \frac{1}{\sqrt{1+(a_0t/c)^2}} \right) dt = (c/a_0)\, arsinh(a_0 \Delta t/c)

Now I know you wanted no hyperbolic functions, but it is almost unavoidable in the proper time calculation. However, there is an alternative in the form of the natural log Ln which is:

t_0 = (c/a)\, arsinh(a_0t/c) = (c/a_0) Ln((at/c)+\gamma) = 1/2*Ln( 20+ 20.025) = 1.845 s

Hyperbolic curves have the form x^2-y^2 = Constant and the Minkowski metric has the same form (dx/dt_0)^2 - (cdt/dt_0)^2 = c^2, so hyperbolic functions will keep popping up.

Some hyperbolic functions can only be expressed in terms of exponential functions and logarithms, but these are transcendental functions too and cannot be expressed in simple algebraic terms.

Proper velocity in S

I will leave this for another post as I am still thinking about it and this post is long enough.

This long post is me gathering my thoughts on the topic and may contain typos/ mistakes/ misunderstandings/ misconceptions so any corrections are welcome.

Having explained your derivations of the equations used, my original question: For a given mass m at rest, what would be the final velocity if a constant force (in the resting FR or S) were to be applied to it, has been answered as well as the general approach to delineating this.

Any texts that cover this as you contributors did? I haven't seen any. Maybe those of Wolfgang Rindler, which starthaus uses, but I don't know which one as he has written several. I am cheap and I don't need the latest text so a cheaper earlier edition such as the first edition of Taylor/Wheeler Spacetime Physics would be ideal.

When I started the original thread, I thought this would be a "wham-bam" quickie amswer but this has resulted in a thread of some 40+ posts with thoughtful responses in these posts (other than mine which were still at the novice level.)

I will start a new thread on hyperbolic functions in relation to the Lorentz transformations. starthaus and DrGreg have used the hyperbolic functions numerous times in proving their points and I must get a working knowledge of them, at least to the level you have gone with times, distances and velocities in accelerated frames.

For starters, given x, t, in S and x', t' in S' then:

x2 - t2 = x'2 - t'2 (if spacelike)
t2 - x2 = t'2 - x'2 (if timelike)

what do you normally use - which hyperbola?
 
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  • #47
starthaus said:
Yes. And this is not a very good definition to begin with because the RHS is a differential while the LHS is not.

I take it...

"RHS" = "Right Hand Side"
"LHS" = "Left Hand Side"

starthaus said:
The standard interpretation follows correctly from the INVARIANCE of the Minkowski metric as follows:

(c d \tau)^2=(cdt)^2-dx^2

I am sure I have shown this before.

I love this one as it leads into my next thread on hyperbolic functions and the Lorentz transformations or Minkowski metric.
 
  • #48
yuiop said:
While checking out your observation, I noticed another interesting relationship.

The slowest time between the two events is the elapsed proper time interval t_i measured by a clock moving inertially between the two events, i.e. t_i = \sqrt{\Delta t^2 - \Delta x^2/c^2}
Now it seems from playing around with my spreadsheet, that the following (without proof) is true:

\Delta x = \frac{1}{2} \alpha t_i^2

which has the same form as the Newtonian equation.

It obviously follows that the constant proper acceleration can be obtained from this simple equation:

\alpha = 2\frac{\Delta x}{t_i^2}

P.S. That should be seconds, not years, to be consistent with the original scenario :wink:

To starthaus - isn't this claim a basic tenet of SR - that (in the timelike area) for inertially moving objects, \tau = SQRT[(delta x)2 - (delta t)2]? I am sure that I have the wrong claim that you speak of.
 
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  • #49
stevmg said:
To starthaus - isn't this claim a basic tenet of SR - that (in the timelike area) for inertially moving objects, \tau = SQRT[(delta x)2 - (delta t)2]? I am sure that I have the wrong claim that you speak of.

The correct derivation starts with:

(c d \tau)^2=(cdt)^2-dx^2

It is important that you understand the differential form. The LHS and RHS are BOTH total differentials.
 
  • #50
starthaus said:
yuiop said:
I clearly defined t_i as \sqrt{\Delta t^2- \Delta x^2/c^2} in post #38: [/tex]
Yes. And this is not a very good definition to begin with because the RHS is a differential while the LHS is not.
Yes, I am guilty of sometimes using just x to mean \Delta x and vice versa, but you do know what I mean from the context. In post 40 you said:

starthaus said:
You must mean

d \tau=\sqrt{ \Delta t^2 - \Delta x^2/c^2}

You are guilty of using a similar mixing of symbols here. d \tau and \Delta \tau do not necessarily mean the same thing. The equation should be either:

d \tau=\sqrt{ dt^2 - dx^2/c^2}

or:

\Delta \tau=\sqrt{ \Delta t^2 - \Delta x^2/c^2}

I hope you understand that for example, \frac{\Delta x}{\Delta t} is not always the same as \frac{dx}{dt}

In the worked acceleration example given in post we had {\Delta x} = 9.5125 and {\Delta t} = 10 so the average velocity of the accelerating object between the two events:

\frac{\Delta x}{\Delta t} = 0.95125c

while the final instantaneous coordinate velocity was found to be:

\frac{dx}{dt} = 0.99875c

Do you see they are not the same thing? One is the average velocity over a non-infinitesimal period while the other is an instantaneous velocity over an infinitesimal period. The distinction is important in an accelerating context.

starthaus said:
The standard interpretation follows correctly from the INVARIANCE of the Minkowski metric as follows:

(c d \tau)^2=(cdt)^2-dx^2

I am sure I have shown you this before.
Please stop saying insulting things like this trying to put me down. That is against the rules of PF. I had used that equation hundreds of time in this forum before you even joined it. You did not "show" me this.

starthaus said:
Definitely wrong since you are effectively writing t=\frac{\Delta x}{c}

Yes, I misquoted some formulas from http://www.xs4all.nl/~johanw/PhysFAQ/Relativity/SR/rocket.html and I have now corrected them in the original post (#38). You are nit-picking about typos and minutia and completely missing the whole point and substance of the physics, which is that the elapsed time on a clock accelerating between two events is not the same as the elapsed time of a clock moving inertially between the same two events. Do you now agree that the after editing, that post #38 is now correct and that you are wrong about the substance and physics of the issue?

starthaus said:
Sure, if you use wrong derivations, it is easy to show anything.

I did not do any derivations in post #38. I was just quoting the standard Minkowski metric and the standard relativistic rocket equations from http://www.xs4all.nl/~johanw/PhysFAQ/Relativity/SR/rocket.html
Admittedly I made several typos in the transcription of the equations, which I hope are now fixed in the original post.
 
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  • #51
yuiop said:
I hope you understand that for example, \frac{\Delta x}{\Delta t} is not always the same as \frac{dx}{dt}

You can't be serious.
I did not do any derivations in post #38. I

You mean, you guessed

\Delta x=\frac{a t_i^2}{2}?

For good reason this is not part of the webpage you are citing ("The Relativistic Rocket"), it is total nonsense as I have showed . If you just guessed it without any derivation, try deriving it. This is all I was asking.
 
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  • #52
starthaus said:
yuiop said:
I hope you understand that for example, \frac{\Delta x}{\Delta t} is not always the same as \frac{dx}{dt}
You can't be serious.
I am serious. Do you disagree?
 
  • #53
yuiop said:
Problem statement:

Proper acceleration = 2c /s.

The x axes of S and S' are parallel to each other and the relative velocity of the frames and the acceleration and the velocity of the accelerated object is parallel to the x axes.

The velocity of accelerating object is v=0 at time t=0 and the object accelerates for 10 seconds as measured in frame S. We will consider two events, one at the start and at one at the end of the acceleration period.

Event 1:
(x1,t1) = (0,0)
(x1',t2') = (0,0)

Event 2:
(x2,t2) = (Δx,10)
(x2',t2') = (Δx', Δt')

\Delta x = (x_2-x_1) = x_2 \quad , \quad \Delta t = (t_2-t_1) = t_2
\Delta x&#039; = (x_2&#039;-x_1&#039;) = x_2&#039; \quad , \quad \Delta t&#039; = (t_2&#039;-t_1&#039;) = t_2&#039;

v is the final velocity of the accelerating object in frame S and is also the relative velocity of frame S' to frame S.

The instantaneous gamma factor at the terminal velocity in frame S

\gamma = \sqrt{1+(a&#039;t/c)^2} = \frac{1}{\sqrt{1-v^2/c^2}} = 20.025

Final coordinate velocity in S

v = \frac{a&#039;t}{\sqrt{1+(a&#039;t/c)^2}} = a&#039;t/\gamma = \frac{2*10}{20.025} = 0.99875c
yuiop said:
Coordinate distance Δx traveled in frame S

\Delta x = (c^2/a)*(\sqrt{(1+(a \Delta t /c)^2)} -1) = (c^2/a)*(\gamma-1) = (1/2)*(20.025-1) = 9.5125
The origen of S' at (t=10) will be colocated with (t=10,x=9.9875) yes?
Considering that the accelerating system started out at v=0 while the S' system was moving at .99875c and the accl. Frame only attains that velocity at the end. how could the accl system end up having traveled almost an equal distance?
After 10 secs S' (.4994,0) will be at S (10,9.9875)
S(0.4994,0) will be located at S' (10,-9.9875) correct?
If this is correct it would seem to follow that event 2 must lie somewhere in the middle between these two events both spatially and temporally.


yuiop said:
Coordinate distance Δx' in the CMIRF (S')

Fram the Lorentz transformation:

\Delta x&#039; = \frac{\Delta x-v \Delta t}{\sqrt{1-v^2/c^2}} = \gamma(\Delta x-v \Delta t) = 20.025*(9.5125-0.99875*10) = -9.5125

You might find it surprising and unintuitive that the distance between the two events is the same in frame S and frame S', except for the sign. I know I did and maybe I made a mistake somewhere. .
A frame traveling 0.9521 relative to both S and S' would end up in the middle.
I.e. v= 0.9512 relative to S ,,,,and v= -0.9512 relative to S' but it could not have traveled 10 secs in either frame.

I may be totally wrong about all this but I think there may be a problem with using the CMIRF as I said last post.


yuiop said:
Proper distance:

Distance is poorly defined in an accelerating reference frame. Proper distance in inertial RFs is normally the distance measured by a ruler between two simultaneous events. Since the two events are not simultaneous in any inertial reference frame in this example it is hard to define a proper distance even in the inertial reference frames. We can however invoke a notion of the invariant interval which can be thought of as the proper distance between events 1 and 2.

(c \Delta t)^2 - \Delta x^2 = (10)^2 - 9.5125^2 = 9.5125 .

yuiop said:
Coordinate elapsed time Δt' in the CMIRF

Using the Lorentz transformation:

\Delta t&#039; = \frac{<br /> \Delta t-v \Delta x/c^2}{\sqrt{1-v^2/c^2}} = \gamma(\Delta t-v\Delta x/c^2) = 20.025*(10-0.99875*9.5125) = 10 s

Again this is a counter-intuitive result. .
yuiop said:
Proper elapsed time:

As above ,,I think there may be a problem here

The proper elapsed time for the accelerating object is clearly defined because it measured by a single clock between the two events. It is derived like this. The total elapsed proper time is the integral of the instantaneous proper time at any instant which is a function of the instantaneous velocity u at any instant, so:

\frac{dt_0}{dt} = \frac{1}{\gamma^2} = \sqrt{1-u^2/c^2} = \frac{1}{\sqrt{1+(a_0\Delta t/c)^2}}

Integrating both sides with respect to t:

\Delta t_0 = \int \left( \frac{1}{\sqrt{1+(a_0t/c)^2}} \right) dt = (c/a_0)\, arsinh(a_0 \Delta t/c)

.
In this situation the elapsed time in S and S' do not really represent elapsed proper time but time as applied at different locations, so the clock desynchronization accounts for most of the difference between local clocks at event 2 and the accelerated systems elapsed proper time , yes?
 
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  • #54
With all this discussion going on from my original thread I do NOT feel that I am such a novice after all!

stevmg
 
  • #55
starthaus said:
yuiop said:
Now it seems from playing around with my spreadsheet, that the following (without proof) is true:

\Delta x = \frac{1}{2} \alpha t_i^2

which has the same form as the Newtonian equation.

It obviously follows that the constant proper acceleration can be obtained from this simple equation:

\alpha = 2\frac{\Delta x}{t_i^2}
This cannot be since:

x=\frac{c^2}{a}(cosh(a \tau/c)-1)

dx=c d\tau sinh(a \tau/c)

starthaus said:
You mean, you guessed

\Delta x=\frac{a t_i^2}{2}?

For good reason this is not part of the webpage you are citing ("The Relativistic Rocket") . If you just guessed it without any derivation, try deriving it. This is all I was asking.
When I first noticed the relationship, it "jumped out" at me when looking at the numbers on a spreadsheet and I did not not have a derivation, so yes in that sense I "guessed it". I now have the derivation as shown below:

Using notation defined thus:

Coordinate distance interval in S = \Delta x = d
Coordinate time interval in S = \Delta t = t
Proper acceleration = \alpha

.. the equation for coordinate distance from http://www.xs4all.nl/~johanw/PhysFAQ/Relativity/SR/rocket.html" is given as:

d = (c^2/\alpha)*(\sqrt{(1+(\alpha t /c)^2)} -1)

\rightarrow \alpha d = \sqrt{c^4+(\alpha t c)^2} - c^2

\rightarrow (\alpha d +c^2)^2 = c^4+(\alpha t c)^2

\rightarrow \alpha^2d^2 + c^4 + 2c^2\alpha d = c^4+\alpha^2 t^2 c^2

\rightarrow \alpha d^2 + 2c^2 d = \alpha t^2 c^2

\rightarrow 2c^2d =\alpha (t^2 c^2 - d^2)

\rightarrow \alpha = \frac{2d}{(t^2 - d^2/c^2)}


Since I defined t_i[/tex] as \sqrt{(t^2 - d^2/c^2) the following statents are true:<br /> <br /> \alpha = \frac{2d}{t_i^2}<br /> <br /> t_i = \sqrt{\frac{2d}{\alpha}}<br /> <br /> d = \frac{1}{2} \, \alpha t_i^2<br /> <br /> It is also an exact solution because I derived it directly from from an exact formula.<br /> <br /> Q.E.D.
 
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  • #56
stevmg said:
With all this discussion going on from my original thread I do NOT feel that I am such a novice after all!

stevmg
Well, acceleration in relativity is not a novice subject, but it is fairly straightforward. :wink:
 
  • #57
yuiop said:
When I first noticed the relationship, it "jumped out" at me when looking at the numbers on a spreadsheet and I did not not have a derivation, so yes in that sense I "guessed it". I now have the derivation as shown below:

Using notation defined thus:

Coordinate distance interval in S = \Delta x = d
Coordinate time interval in S = \Delta t = t
Proper acceleration = \alpha

.. the equation for coordinate distance from http://www.xs4all.nl/~johanw/PhysFAQ/Relativity/SR/rocket.html" is given as:

d = (c^2/\alpha)*(\sqrt{(1+(\alpha t /c)^2)} -1)

\rightarrow \alpha d = \sqrt{c^4+(\alpha t c)^2} - c^2

\rightarrow (\alpha d +c^2)^2 = c^4+(\alpha t c)^2

\rightarrow \alpha^2d^2 + c^4 + 2c^2\alpha d = c^4+\alpha^2 t^2 c^2

\rightarrow \alpha d^2 + 2c^2 d = \alpha t^2 c^2

\rightarrow 2c^2d =\alpha (t^2 c^2 - d^2)

\rightarrow \alpha = \frac{2d}{(t^2 - d^2/c^2)}


Since I defined t_i[/tex] as \sqrt{(t^2 - d^2/c^2) the following statents are true:<br /> <br /> \alpha = \frac{2d}{t_i^2}<br /> <br /> t_i = \sqrt{\frac{2d}{\alpha}}<br /> <br /> d = \frac{1}{2} \, \alpha t_i^2<br /> <br /> It is also an exact solution because I derived it directly from from an exact formula.<br /> <br /> Q.E.D.
<br /> <br /> Beautiful!<br /> <br /> How did you get the &quot;quote within a quote&quot; as you did with this (your quoted post was quoted within starthaus&#039;s quote.)
 
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  • #58
stevmg said:
Beautiful!

How did you get the "quote within a quote" as you did with this (your quoted post was quoted within starthaus's quote.)

You can do it like this:

PHP:
[quote="starthaus, post: 2873083"]

[quote="yuiop, post: 2873062"]
I hope you understand that for example,
  [tex]\frac{\Delta x}{\Delta t}[/tex] 
is not always the same as
 [tex]\frac{dx}{dt}[/tex] 
[/QUOTE]

You can't be serious.
[/QUOTE]

To get:

starthaus said:
yuiop said:
I hope you understand that for example, \frac{\Delta x}{\Delta t}
is not always the same as \frac{dx}{dt}

You can't be serious.

or:

PHP:
[quote="yuiop, post: 2873062"]
I hope you understand that for example,
  [tex]\\frac{\Delta x}{\Delta t}[/tex] 
is not always the same as
 [tex]\frac{dx}{dt}[/tex] 

[quote="starthaus, post: 2873083"]
You can't be serious.
[/QUOTE]
[/QUOTE]

to get:

yuiop said:
I hope you understand that for example, \frac{\Delta x}{\Delta t}
is not always the same as \frac{dx}{dt}

starthaus said:
You can't be serious.
I wrapped it in PHP tags so that you can actually see the quote tags. Just use the multi quote feature and copy and paste to nest the quotes inside each other.
 
  • #59
yuiop said:
You can do it like this:

PHP:

To get:



or:

PHP:

to get:





I wrapped it in PHP tags so that you can actually see the quote tags. Just use the multi quote feature and copy and paste to nest the quotes inside each other.

Thanks...

stevmg
 
  • #60
Austin0 said:
The origen of S' at (t=10) will be colocated with (t=10,x=9.9875) yes?

Yep, that makes sense if frame S' is traveling at 0.99875c and if the origins of S and S' were initially collocated.

Austin0 said:
Considering that the accelerating system started out at v=0 while the S' system was moving at .99875c and the accl. Frame only attains that velocity at the end. how could the accl system end up having traveled almost an equal distance?

The acceleration is extreme. In post #28 , I calculated that the accelerating object gets to nearly 0.8944c in the first second.

The accelerating object travels a distance of 9.5125 in 10 seconds so its average velocity in S is 0.95125c so it is not that much slower than the 0.99875c velocity of the CMIRF.

Austin0 said:
After 10 secs S' (.4994,0) will be at S (10,9.9875)
S(0.4994,0) will be located at S' (10,-9.9875) correct?
If this is correct it would seem to follow that event 2 must lie somewhere in the middle between these two events both spatially and temporally.

(t,x) = (10,9.5125) is event 2 in frame S and (t',x') = (10,-9.5125) is the same event 2 in frame S'. Where is this event 2 that lies somewhere between those events that you speak of?

You can't simply apply the gamma factor to the time in S to get the time in S' as 0.4994 because the initial vent and the final event are not at the same place in either reference frame. It is basically a simultaneity issue.

Austin0 said:
A frame traveling 0.9521 relative to both S and S' would end up in the middle.
I.e. v= 0.9512 relative to S ,,,,and v= -0.9512 relative to S' but it could not have traveled 10 secs in either frame.
The figure you have calculated for a reference frame that sees the origins of S and S' going away at equal speeds in opposite directions appears to be correct. This new frame would not appear to be in the middle in either frame S or S'. I am not sure why you think that is significant.

Austin0 said:
I may be totally wrong about all this but I think there may be a problem with using the CMIRF as I said last post.
All I can say is that using the CMIRF concept is a perfectly standard method in textbooks. Well at least I think it would be if I had any textbooks :-p (it appears to be perfectly standard in serious online references anyway.)

Austin0 said:
In this situation the elapsed time in S and S' do not really represent elapsed proper time but time as applied at different locations, so the clock desynchronization accounts for most of the difference between local clocks at event 2 and the accelerated systems elapsed proper time , yes?
Correct again. That is why I have always referred to the elapsed times in S and S' as coordinate times rather than as proper times.
 
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